{"created":"2023-06-20T15:13:59.637178+00:00","id":43963,"links":{},"metadata":{"_buckets":{"deposit":"f6108d6f-2724-464d-8a21-454498630923"},"_deposit":{"created_by":1,"id":"43963","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43963"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043963","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466692","466698","466696","466690","466693","466699","466695","466700","466694","466697","466691","466689"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1979-03","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"20","bibliographicVolumeNumber":"380","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0380000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TM-380","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者(英)","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所機体第二部"},{"subitem_text_value":"航空宇宙技術研究所機体第二部"},{"subitem_text_value":"航空宇宙技術研究所機体第二部"},{"subitem_text_value":"航空宇宙技術研究所機体第二部"},{"subitem_text_value":"航空宇宙技術研究所機体第二部"},{"subitem_text_value":"航空宇宙技術研究所機体第二部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"浜口, 泰正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"飯田, 宗四郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中井, 暎一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"寺田, 博之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"角田, 義秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塙, 武敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HAMAGUCHI, Yasumasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IIDA, Soshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAI, Eiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hiroyuki, Terada","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAKUTA, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HANAWA, Taketoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-28"}],"displaytype":"detail","filename":"naltm00380.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00380.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43963/files/naltm00380.pdf"},"version_id":"9dc04ca8-ad8a-4203-8fde-29838347218e"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"液体ロケット燃料タンク構造用材料の極低温(4K)における強度特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"液体ロケット燃料タンク構造用材料の極低温(4K)における強度特性"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43963","relation_version_is_last":true,"title":["液体ロケット燃料タンク構造用材料の極低温(4K)における強度特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:04:55.517704+00:00"}